ATE337959T1 - Verfahren zum verringern der aerodynamischen kräfte auf ein flugzeughöhenruder während des abhebens - Google Patents
Verfahren zum verringern der aerodynamischen kräfte auf ein flugzeughöhenruder während des abhebensInfo
- Publication number
- ATE337959T1 ATE337959T1 AT04292844T AT04292844T ATE337959T1 AT E337959 T1 ATE337959 T1 AT E337959T1 AT 04292844 T AT04292844 T AT 04292844T AT 04292844 T AT04292844 T AT 04292844T AT E337959 T1 ATE337959 T1 AT E337959T1
- Authority
- AT
- Austria
- Prior art keywords
- aerodynamic forces
- during take
- reducing aerodynamic
- elevator during
- aircraft elevator
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/02—Tailplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Bridges Or Land Bridges (AREA)
- Radar Systems Or Details Thereof (AREA)
- Numerical Control (AREA)
- Tires In General (AREA)
- Lift-Guide Devices, And Elevator Ropes And Cables (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0314951A FR2864022B1 (fr) | 2003-12-19 | 2003-12-19 | Procede pour la reduction des charges aerodynamiques appliquees aux gouvernes de profondeur d'un aeronef lors d'un decollage. |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE337959T1 true ATE337959T1 (de) | 2006-09-15 |
Family
ID=34508704
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT04292844T ATE337959T1 (de) | 2003-12-19 | 2004-12-01 | Verfahren zum verringern der aerodynamischen kräfte auf ein flugzeughöhenruder während des abhebens |
Country Status (7)
Country | Link |
---|---|
US (1) | US7264201B2 (de) |
EP (1) | EP1544100B1 (de) |
AT (1) | ATE337959T1 (de) |
CA (1) | CA2489794C (de) |
DE (1) | DE602004002181T2 (de) |
ES (1) | ES2270316T3 (de) |
FR (1) | FR2864022B1 (de) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110150812A1 (en) * | 2009-12-22 | 2011-06-23 | L'oreal S.A. | Natural conditioning cosmetic compositions |
ES2623000T3 (es) * | 2012-07-16 | 2017-07-10 | Airbus Operations, S.L. | Superficie sustentadora de aeronave con una distribución de flecha variable a lo largo de la envergadura |
RU2593178C1 (ru) * | 2015-06-05 | 2016-07-27 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Аэродинамический руль |
RU2615605C1 (ru) * | 2015-11-02 | 2017-04-05 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | Самолет с адаптивным цельноповоротным стабилизатором |
CA3022226A1 (en) * | 2016-04-25 | 2017-11-02 | Bombardier Inc. | Aircraft pitch control system with electronically geared elevator |
US10816998B2 (en) * | 2017-09-18 | 2020-10-27 | The Boeing Company | Airplane takeoff trims utilizing both stabilizers and elevators |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1827304A (en) * | 1928-03-19 | 1931-10-13 | Thurston Albert Peter | Means for controlling aircraft, submarines, and like totally immersed craft or structures |
US3000595A (en) * | 1959-07-21 | 1961-09-19 | Boeing Co | Elevator tab convertible from an antibalance tab to an assist tab |
US3363862A (en) * | 1966-10-20 | 1968-01-16 | Gen Dynamics Corp | Variable camber longitudinal control system for aircraft |
US4034334A (en) * | 1975-07-14 | 1977-07-05 | The Boeing Company | Airfoil position range selecting, indicating and warning system for an aircraft |
US4043523A (en) * | 1976-03-11 | 1977-08-23 | Ball Brothers Research Corporation | Apparatus for aircraft pitch trim |
US5002240A (en) * | 1985-08-19 | 1991-03-26 | Pont Anthony A Du | Aircraft pitch control system |
US4825375A (en) * | 1985-12-23 | 1989-04-25 | Boeing Company | Apparatus and methods for apportioning commands between aircraft flight control surfaces |
FR2864023B1 (fr) * | 2003-12-19 | 2006-03-03 | Airbus France | Procede pour ameliorer la manoeuvrabilite d'un aeronef lors d'une ressource. |
-
2003
- 2003-12-19 FR FR0314951A patent/FR2864022B1/fr not_active Expired - Fee Related
-
2004
- 2004-12-01 DE DE602004002181T patent/DE602004002181T2/de active Active
- 2004-12-01 EP EP04292844A patent/EP1544100B1/de not_active Not-in-force
- 2004-12-01 AT AT04292844T patent/ATE337959T1/de not_active IP Right Cessation
- 2004-12-01 ES ES04292844T patent/ES2270316T3/es active Active
- 2004-12-03 US US11/002,067 patent/US7264201B2/en active Active
- 2004-12-07 CA CA2489794A patent/CA2489794C/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
ES2270316T3 (es) | 2007-04-01 |
CA2489794A1 (fr) | 2005-06-19 |
EP1544100B1 (de) | 2006-08-30 |
EP1544100A1 (de) | 2005-06-22 |
US7264201B2 (en) | 2007-09-04 |
FR2864022A1 (fr) | 2005-06-24 |
US20050178899A1 (en) | 2005-08-18 |
FR2864022B1 (fr) | 2006-03-03 |
DE602004002181T2 (de) | 2007-09-20 |
CA2489794C (fr) | 2011-11-22 |
DE602004002181D1 (de) | 2006-10-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |